Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44

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ISBN 13 :
Total Pages : 430 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 by : Paige B. Burbank

Download or read book Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 written by Paige B. Burbank and published by . This book was released on 1962 with total page 430 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Measurements on a Flat Plate and Attached Protuberances in a Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44

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ISBN 13 :
Total Pages : 246 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer Measurements on a Flat Plate and Attached Protuberances in a Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 by : Robert L. Stallings

Download or read book Heat-transfer Measurements on a Flat Plate and Attached Protuberances in a Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 written by Robert L. Stallings and published by . This book was released on 1964 with total page 246 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Measurements on a Flat Plate with Attached Protuberances in a Turbulent Boundary Layer at Mach Numbers of 2.49, 3.51, and 4.44

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ISBN 13 :
Total Pages : 114 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer Measurements on a Flat Plate with Attached Protuberances in a Turbulent Boundary Layer at Mach Numbers of 2.49, 3.51, and 4.44 by : Lana Murphy Couch

Download or read book Heat-transfer Measurements on a Flat Plate with Attached Protuberances in a Turbulent Boundary Layer at Mach Numbers of 2.49, 3.51, and 4.44 written by Lana Murphy Couch and published by . This book was released on 1966 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (689 download)

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Book Synopsis Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 by : Paige B. Burbank

Download or read book Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 written by Paige B. Burbank and published by . This book was released on 1962 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44

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ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 by : Earl A. Price

Download or read book Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 written by Earl A. Price and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer on a Flat Plate with Attached Protuberances in a Turbulant Boundary Layer at Mach Number of 2.49. 3.51, and 4.44

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ISBN 13 :
Total Pages : 110 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Heat-transfer on a Flat Plate with Attached Protuberances in a Turbulant Boundary Layer at Mach Number of 2.49. 3.51, and 4.44 by : Lana Murphy Couch

Download or read book Heat-transfer on a Flat Plate with Attached Protuberances in a Turbulant Boundary Layer at Mach Number of 2.49. 3.51, and 4.44 written by Lana Murphy Couch and published by . This book was released on 1966 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44

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ISBN 13 :
Total Pages : 423 pages
Book Rating : 4.:/5 (761 download)

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Book Synopsis Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 by : Paige B. Burbank

Download or read book Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 written by Paige B. Burbank and published by . This book was released on 1962 with total page 423 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution by : Raul J. Conti

Download or read book Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution written by Raul J. Conti and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurement on Attaches Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44

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ISBN 13 :
Total Pages : 423 pages
Book Rating : 4.:/5 (249 download)

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Book Synopsis Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurement on Attaches Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 by : Paige B. Burbank

Download or read book Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurement on Attaches Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 written by Paige B. Burbank and published by . This book was released on 1962 with total page 423 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution by : Raul Jorge Conti

Download or read book Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution written by Raul Jorge Conti and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Pressures and Turbulent Heat-transfer Coefficients Associated with Sinusoidal Protuberances on a Flat Plate at a Mach Number of 3

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Experimental Pressures and Turbulent Heat-transfer Coefficients Associated with Sinusoidal Protuberances on a Flat Plate at a Mach Number of 3 by : Charles P. Shore

Download or read book Experimental Pressures and Turbulent Heat-transfer Coefficients Associated with Sinusoidal Protuberances on a Flat Plate at a Mach Number of 3 written by Charles P. Shore and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Preliminary Results from a Free-flight Investigation of Boundary-layer Transition and Heat Transfer on a Highly Polished 8-inch-diameter Hemisphere-cylinder at Mach Numbers Up to 3 and Reynolds Numbers Based on a Length of 1 Foot Up to 17.7 X 106

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Preliminary Results from a Free-flight Investigation of Boundary-layer Transition and Heat Transfer on a Highly Polished 8-inch-diameter Hemisphere-cylinder at Mach Numbers Up to 3 and Reynolds Numbers Based on a Length of 1 Foot Up to 17.7 X 106 by : James R. Hall

Download or read book Preliminary Results from a Free-flight Investigation of Boundary-layer Transition and Heat Transfer on a Highly Polished 8-inch-diameter Hemisphere-cylinder at Mach Numbers Up to 3 and Reynolds Numbers Based on a Length of 1 Foot Up to 17.7 X 106 written by James R. Hall and published by . This book was released on 1957 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Measurements of Aerodynamic Heat Transfer in Turbulent Separated Regions at a Mach Number of 1.8

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Measurements of Aerodynamic Heat Transfer in Turbulent Separated Regions at a Mach Number of 1.8 by : Benjamine J. Garland

Download or read book Measurements of Aerodynamic Heat Transfer in Turbulent Separated Regions at a Mach Number of 1.8 written by Benjamine J. Garland and published by . This book was released on 1958 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 by : Robert L. O'Neal

Download or read book Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 written by Robert L. O'Neal and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0

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ISBN 13 :
Total Pages : 106 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0 by : Paul F. Holloway

Download or read book An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0 written by Paul F. Holloway and published by . This book was released on 1965 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Survey of Boundary Layer Heat Transfer at High Velocities and High Temperatures

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ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Survey of Boundary Layer Heat Transfer at High Velocities and High Temperatures by : Ernst Rudolf Georg Eckert

Download or read book Survey of Boundary Layer Heat Transfer at High Velocities and High Temperatures written by Ernst Rudolf Georg Eckert and published by . This book was released on 1960 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Heat Transfer Through Laminar and Turbulent Boundary Layers on a Cooled Flat Plate at a Mach Number of 2.4

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ISBN 13 :
Total Pages : 734 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Experimental Investigation of Heat Transfer Through Laminar and Turbulent Boundary Layers on a Cooled Flat Plate at a Mach Number of 2.4 by : Ellis G. Slack

Download or read book Experimental Investigation of Heat Transfer Through Laminar and Turbulent Boundary Layers on a Cooled Flat Plate at a Mach Number of 2.4 written by Ellis G. Slack and published by . This book was released on 1952 with total page 734 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel tests of the heat-transfer characteristics for laminar and turbulent boundary layers on a cooled flat plate were conducted at a Mach number of 2.4. Data were obtained for a Reynolds number range of 150.000 to 3,000.000 and for a surface-temperature range of -40 degrees F to 45 degrees F with recovery temperature of the order of 65 degrees F. The temperature-recovery factors agreed well with previous flat-plate reslts. The heat-transfer results were obtained with negative temperature gradients along the surface and, when related to the constant-surface-temperature case, were, in general, in good agreement with theory.